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Inlet flow angle determination of transonic compressor cascade

Steinert, W. and Fuchs, R. and Starken, H. (1991) Inlet flow angle determination of transonic compressor cascade. 36th ASME International Gas Turbine and Aeroengine Congress and Exposition, Orlando (USA), 03.-06.06.91.

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Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1991,
Title:Inlet flow angle determination of transonic compressor cascade
Authors:
AuthorsInstitution or Email of Authors
Steinert, W.UNSPECIFIED
Fuchs, R.UNSPECIFIED
Starken, H.UNSPECIFIED
Date:1991
Status:Published
Event Title:36th ASME International Gas Turbine and Aeroengine Congress and Exposition, Orlando (USA), 03.-06.06.91
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L SI - Versuchs- und Simulationstechniken
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:12

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